Acceleration along the body-fixed Y axis of the satellite. Input is unitless but is multiplied by 1.0e-12 m/s2 to yield an acceleration perpendicular to the sun-to-satellite line. Also known as K2, the nominally value is in the range of -1 < YBias < 1.
Read-write property
[Visual Basic .NET] |
---|
Public Property YBias() As Double |
[C#] |
---|
public double YBias {get; set;} |
[Managed C++] |
---|
public: __property double get_YBias(); |
[Unmanaged C++] |
---|
public: HRESULT get_YBias( double * pVal ); public: HRESULT put_YBias( double YBias ); |
[Java] |
---|
public double getYBias(); public void setYBias( double ); |